About Gemini 6

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Gemini VI-A
, Gemini VI-A (foreground) and Gemini VII make the first rendezvous in orbit between two manned spacecraft
Operator
NASA
COSPAR ID
1965-104A
SATCAT №
1839
Mission duration
1 day, 1 hour, 51 minutes, 24 seconds
Distance travelled
694,415 kilometers (374,954 nautical miles)
Orbits completed
16
Spacecraft properties
Spacecraft
Gemini SC6
Manufacturer
McDonnell
Launch mass
3,546 kilograms (7,818 lb)
Crew
Crew size
2
Members
Walter M. Schirra, Jr., Thomas P. Stafford
Start of mission
Launch date
December 15, 1965, 13:37:26 (1965-12-15UTC13:37:26Z) UTC
Rocket
Titan II GLV, s/n 62-12561
Launch site
Cape Canaveral LC-19
End of mission
Landing date
December 16, 1965, 15:28:50 (1965-12-16UTC15:28:51Z) UTC
Landing site
North Atlantic Ocean, 23°35′N 67°50′W﻿ / ﻿23.583°N 67.833°W﻿ / 23.583; -67.833
Orbital parameters
Reference system
Geocentric
Regime
Low Earth
Perigee
161 kilometers (87 nautical miles)
Apogee
259.4 kilometers (140.1 nautical miles)
Inclination
28.97 degrees
Period
88.7 minutes
, (L-R) Stafford, Schirra
Project Gemini
← Gemini 7
Gemini 8 →
Gemini 6A (officially Gemini VI-A) was a 1965 manned United States spaceflight in NASA's Gemini program. The mission achieved the first manned rendezvous with another spacecraft, its sister Gemini 7. Although the Soviet Union had twice previously launched simultaneous pairs of Vostok spacecraft, these established radio contact with, but came no closer than several kilometers of each other, while the Gemini 6 and 7 spacecraft came as close as one foot (30 cm) and could have docked had they been so equipped.
Gemini 6A was the fifth manned Gemini flight, the 13th manned American flight, and the 21st manned spaceflight of all time (includes X-15 flights over 100 kilometers (54 nautical miles).
Contents
1 Crew
1.1 Backup crew,
1.2 Support crew,
,
2 Mission parameters
2.1 Stationkeeping with GT-7,
,
3 Objective
3.1 Original mission cancelled,
,
4 Flight
4.1 First launch attempt,
4.2 Rendezvous,
4.3 A Christmas surprise,
4.4 Reentry,
,
5 Insignia,
6 Spacecraft location,
7 See also,
8 References,
9 External links,
Crew:
Position
Astronaut
Command Pilot
Walter M. Schirra, Jr.,
Second spaceflight
Pilot
Thomas P. Stafford,
First spaceflight
Backup crew:
Position
Astronaut
Command Pilot
Virgil I. Grissom
Pilot
John W. Young
Support crew:
Alan L. Bean (Cape CAPCOM),
Elliot M. See, Jr. (Houston CAPCOM),
Eugene A. Cernan (Houston CAPCOM),
Charles A. Bassett II (Houston CAPCOM),
Mission parameters:
Mass: 3,546 kilograms (7,818 lb),
Perigee: 161 kilometers (100 miles),
Apogee: 259.4 kilometers (161.2 miles),
Inclination: 28.97°,
Period: 88.7 min,
Stationkeeping with GT-7:
Start: December 15, 1965 19:33 UTC,
End: December 16, 1965 00:52 UTC,
Objective:
The original Gemini 6 mission, scheduled for launch on October 25, 1965 at 12:41 pm EDT, had a planned mission duration of 46 hours 47 minutes, completing a total of 29 orbits. It was to land in the western Atlantic Ocean south of Bermuda.
The mission was to include four dockings with the Agena Target Vehicle. The first docking was scheduled for 5 hours 40 minutes into the mission. The second at 7 hours 45 minutes, the third at 9 hours 40 minutes and the fourth and final docking at 10 hours 5 minutes into the mission. The final undocking would take place at 18 hours 20 minutes into the mission.
At 23 hours 55 minutes into the mission, while the spacecraft passed over White Sands, New Mexico, the crew was to attempt to observe a laser beam originating from the ground.
The retro rockets were scheduled to be fired at 46 hours 10 minutes into the mission over the Pacific Ocean on the 29th orbit.
Original mission plans also included the first live television coverage of the recovery of a US spacecraft at sea from the recovery ship, the US aircraft carrier Wasp. The Wasp was fitted with ground station equipment by ITT to relay live television, via the Intelsat I (nicknamed the "Early Bird") satellite.
Original mission cancelled:
On October 25, 1965, Schirra and Stafford boarded their Gemini 6 craft to prepare for launch. Fifteen minutes later, the unmanned Atlas-Agena target vehicle was launched. After a successful burn of the Atlas booster, the Agena's secondary engines fired to separate it from the Atlas. But immediately after the Agena's primary engine fired at the six minute mark in its flight, telemetry was lost. A catastrophic failure apparently caused the vehicle to explode, as Range Safety was tracking multiple pieces of debris falling into the Atlantic Ocean. After 50 minutes, the Gemini launch was canceled.
After reviewing the situation, NASA decided to launch an alternate Gemini 6A mission, eight days after the launch of Frank Borman's and Jim Lovell's Gemini 7. Six-A would perform the first rendezvous using 7 as the target, though it could not dock. The crews also discussed the possibility that Stafford might do an EVA from 6A to 7, swapping places with Lovell, but Borman objected, pointing out that it would require Lovell to wear an uncomfortable EVA suit on a long-duration mission.
Gemini 6 Target Vehicle Info
Agena
GATV-5002
Mass
3,261 kilograms (7,189 lb), 7800 lbs.
Launch site
LC-14
Launch date
October 25, 1965
Launch time
15:00:04 UTC
Exploded
15:06:20 UTC
Flight:
First launch attempt:
The first attempt to launch the 6A mission (second attempt for Gemini spacecraft No. 6) was on December 12, 1965 at 9:54 a.m. EST. All went well right up to ignition--in fact the engines did ignite, but then a plug fell out of the bottom of the rocket, starting the onboard computer. This was not meant to happen until the rocket had actually lifted off, and the onboard computer detected no upward motion, causing it to abort the launch. At this point mission rules called for a pad abort to get the astronauts away from the rocket as quickly as possible, as it would explode on impact with the pad if lifted and fell even the smallest distance.
The Gemini spacecraft used ejection seats for this purpose instead of a capsule escape rocket system as had been used on Project Mercury. The ejection seats were designed to be used only in flight, and trying to use them on the pad would have been extremely dangerous and probably fatal, as Schirra and Stafford would have fallen about 10 stories to the ground without benefit of their parachutes, which would have been ineffective at that height. Since neither had detected any upward motion, Schirra made the decision not to eject.
The Martin and Air Force teams who erected and tested the rocket found that some plugs on the rocket were able to pull out more easily than others. They replaced them with ones that were harder to pull out, and a safety wire was added to make sure that the rocket had lifted off.
However, another problem was found as the engineers examined the thrust versus time graph. They found that the thrust rose nominally but started to decrease before the plug had fallen out. Through the night, engineers examined the rocket engine piece by piece until they found that a plastic cover had been left in the gas generator port. With this problem solved, the rocket and spacecraft were rescheduled for a launch three days after the first attempt.
Rendezvous:
The second attempt to launch the 6A mission (third attempt for Gemini spacecraft No. 6) was successful on December 15 at 8:37:26 a.m. EST. All went well through launch and ascent and the crew entered a 161 by 259 kilometers orbit, or as per the actual flight specifications, a 100 by 161 nautical mile orbit.
The plan called for the rendezvous to take place on the fourth orbit of Gemini 6. Their first burn came 94 minutes after launch when they increased their speed by 5 meters per second, 16½ feet per second. Due to their lower orbit they were gaining on Gemini 7 and were only 730 miles, (or 1,175 kilometers), behind. The next burn was at 2 hours and 18 minutes when Gemini 6A made a phase adjustment to put them on the same orbital inclination as Gemini 7. They now only trailed by 483 kilometers, (300 miles).
The radar on Gemini 6 first made contact with Gemini 7 at 3 hours and 15 minutes when they were 434 kilometers (270 miles) away. A third burn put them into a 168 x 170 mile (270 by 274 kilometer) orbit. As they slowly gained, Schirra put Gemini 6's computer in charge of the rendezvous. At 5 hours and 4 minutes he saw a bright star that he thought was Sirius, but this was in fact Gemini 7.
After several more burns the two spacecraft were only 130 feet (40 meters) apart. The burns had only used 112 lbs. (51 kilograms) of fuel on Gemini 6, giving plenty of fuel for some fly-arounds. During the next 270 minutes the crews moved as close as 1 foot, (30 centimeters), talking over the radio. At one stage the spacecraft were stationkeeping so well that neither crew had to make any burns for 20 minutes.
As the sleep periods approached, Gemini 6 made a separation burn and slowly drifted out to 10 miles (16 kilometers). This ensured that there would not be any accidental collisions in the night.
A Christmas surprise:
But before everyone went to sleep, the crew of Gemini 6 had a surprise for everyone:
Gemini VII, this is Gemini VI_ We have an object, looks like a satellite going from north to south, up in a polar orbit. He's in a very low trajectory traveling from north to south and has a very high climbing ratio. It looks like it might even be a ... Very low. Looks like he mlght be going to reenter soon. Stand by one ... You might just let me try to pick up that thing.
At that point, the sound of "Jingle Bells" was heard played on an 8-note Hohner "Little Lady" harmonica and a handful of small bells. The Smithsonian Institution claims these were the first musical instruments played in space and keeps the instruments on display.
Reentry:
Gemini 6 reentered the next day, landing within 18 kilometers (11 miles) of the planned site northeast of Turks and Caicos in the Atlantic Ocean, the first truly accurate reentry. It was also the first recovery to be televised live, through a transportable satellite earth station developed by ITT on the deck of the recovery aircraft carrier USS Wasp.
The Gemini 7 and 6A missions were supported by the following U.S. Department of Defense resources: 10,125 personnel, 125 aircraft and 16 ships.
Insignia:
Walter Schirra explained the patch in the book All We Did Was Fly to the Moon:
The Gemini 6 patch is hexagonal in shape, reflecting the mission number; and the spacecraft trajectory also traces out the number "6". The Gemini 6 spacecraft is shown superimposed on the "twin stars" Castor and Pollux, for "Gemini".
I designed the patch to locate in the sixth hour of celestial right ascension. This was the predicted celestial area where the rendezvous should occur (in the constellation Orion). It finally did occur there.
The original patch had called the flight GTA-6 (for Gemini-Titan-Agena) and showed the Gemini craft chasing an Agena. It was changed when the mission was altered to depict two Gemini spacecraft.
Spacecraft location:
The spacecraft is currently on display at the Oklahoma History Center in Oklahoma City, after having been on display at the Omniplex Science Museum elsewhere in the city. It is on a long term loan from the Smithsonian Institution. Before coming to Oklahoma, the spacecraft was displayed at the St. Louis Science Center in St. Louis, Missouri.

This article needs additional citations for verification. Please help improve this article by adding citations to reliable sources. Unsourced material may be challenged and removed. (May 2009) Gemini VI-A , Gemini VI-A (foreground) and Gemini VII make the first rendezvous in orbit between two manned spacecraft Operator NASA COSPAR ID 1965-104A SATCAT № 1839 Mission duration 1 day, 1 hour, 51 minutes, 24 seconds Distance travelled 694,415 kilometers (374,954 nautical miles) Orbits completed 16 Spacecraft properties Spacecraft Gemini SC6 Manufacturer McDonnell Launch mass 3,546 kilograms (7,818 lb) Crew Crew size 2 Members Walter M. Schirra, Jr., Thomas P. Stafford Start of mission Launch date December 15, 1965, 13:37:26 (1965-12-15UTC13:37:26Z) UTC Rocket Titan II GLV, s/n 62-12561 Launch site Cape Canaveral LC-19 End of mission Landing date December 16, 1965, 15:28:50 (1965-12-16UTC15:28:51Z) UTC Landing site North Atlantic Ocean, 23°35′N 67°50′W﻿ / ﻿23.583°N 67.833°W﻿ / 23.583; -67.833 Orbital parameters Reference system Geocentric Regime Low Earth Perigee 161 kilometers (87 nautical miles) Apogee 259.4 kilometers (140.1 nautical miles) Inclination 28.97 degrees Period 88.7 minutes , (L-R) Stafford, Schirra Project Gemini ← Gemini 7 Gemini 8 → Gemini 6A (officially Gemini VI-A) was a 1965 manned United States spaceflight in NASA's Gemini program. The mission achieved the first manned rendezvous with another spacecraft, its sister Gemini 7. Although the Soviet Union had twice previously launched simultaneous pairs of Vostok spacecraft, these established radio contact with, but came no closer than several kilometers of each other, while the Gemini 6 and 7 spacecraft came as close as one foot (30 cm) and could have docked had they been so equipped. Gemini 6A was the fifth manned Gemini flight, the 13th manned American flight, and the 21st manned spaceflight of all time (includes X-15 flights over 100 kilometers (54 nautical miles). Contents 1 Crew 1.1 Backup crew, 1.2 Support crew, , 2 Mission parameters 2.1 Stationkeeping with GT-7, , 3 Objective 3.1 Original mission cancelled, , 4 Flight 4.1 First launch attempt, 4.2 Rendezvous, 4.3 A Christmas surprise, 4.4 Reentry, , 5 Insignia, 6 Spacecraft location, 7 See also, 8 References, 9 External links, Crew: Position Astronaut Command Pilot Walter M. Schirra, Jr., Second spaceflight Pilot Thomas P. Stafford, First spaceflight Backup crew: Position Astronaut Command Pilot Virgil I. Grissom Pilot John W. Young Support crew: Alan L. Bean (Cape CAPCOM), Elliot M. See, Jr. (Houston CAPCOM), Eugene A. Cernan (Houston CAPCOM), Charles A. Bassett II (Houston CAPCOM), Mission parameters: Mass: 3,546 kilograms (7,818 lb), Perigee: 161 kilometers (100 miles), Apogee: 259.4 kilometers (161.2 miles), Inclination: 28.97°, Period: 88.7 min, Stationkeeping with GT-7: Start: December 15, 1965 19:33 UTC, End: December 16, 1965 00:52 UTC, Objective: The original Gemini 6 mission, scheduled for launch on October 25, 1965 at 12:41 pm EDT, had a planned mission duration of 46 hours 47 minutes, completing a total of 29 orbits. It was to land in the western Atlantic Ocean south of Bermuda. The mission was to include four dockings with the Agena Target Vehicle. The first docking was scheduled for 5 hours 40 minutes into the mission. The second at 7 hours 45 minutes, the third at 9 hours 40 minutes and the fourth and final docking at 10 hours 5 minutes into the mission. The final undocking would take place at 18 hours 20 minutes into the mission. At 23 hours 55 minutes into the mission, while the spacecraft passed over White Sands, New Mexico, the crew was to attempt to observe a laser beam originating from the ground. The retro rockets were scheduled to be fired at 46 hours 10 minutes into the mission over the Pacific Ocean on the 29th orbit. Original mission plans also included the first live television coverage of the recovery of a US spacecraft at sea from the recovery ship, the US aircraft carrier Wasp. The Wasp was fitted with ground station equipment by ITT to relay live television, via the Intelsat I (nicknamed the "Early Bird") satellite. Original mission cancelled: On October 25, 1965, Schirra and Stafford boarded their Gemini 6 craft to prepare for launch. Fifteen minutes later, the unmanned Atlas-Agena target vehicle was launched. After a successful burn of the Atlas booster, the Agena's secondary engines fired to separate it from the Atlas. But immediately after the Agena's primary engine fired at the six minute mark in its flight, telemetry was lost. A catastrophic failure apparently caused the vehicle to explode, as Range Safety was tracking multiple pieces of debris falling into the Atlantic Ocean. After 50 minutes, the Gemini launch was canceled. After reviewing the situation, NASA decided to launch an alternate Gemini 6A mission, eight days after the launch of Frank Borman's and Jim Lovell's Gemini 7. Six-A would perform the first rendezvous using 7 as the target, though it could not dock. The crews also discussed the possibility that Stafford might do an EVA from 6A to 7, swapping places with Lovell, but Borman objected, pointing out that it would require Lovell to wear an uncomfortable EVA suit on a long-duration mission. Gemini 6 Target Vehicle Info Agena GATV-5002 Mass 3,261 kilograms (7,189 lb), 7800 lbs. Launch site LC-14 Launch date October 25, 1965 Launch time 15:00:04 UTC Exploded 15:06:20 UTC Flight: First launch attempt: The first attempt to launch the 6A mission (second attempt for Gemini spacecraft No. 6) was on December 12, 1965 at 9:54 a.m. EST. All went well right up to ignition--in fact the engines did ignite, but then a plug fell out of the bottom of the rocket, starting the onboard computer. This was not meant to happen until the rocket had actually lifted off, and the onboard computer detected no upward motion, causing it to abort the launch. At this point mission rules called for a pad abort to get the astronauts away from the rocket as quickly as possible, as it would explode on impact with the pad if lifted and fell even the smallest distance. The Gemini spacecraft used ejection seats for this purpose instead of a capsule escape rocket system as had been used on Project Mercury. The ejection seats were designed to be used only in flight, and trying to use them on the pad would have been extremely dangerous and probably fatal, as Schirra and Stafford would have fallen about 10 stories to the ground without benefit of their parachutes, which would have been ineffective at that height. Since neither had detected any upward motion, Schirra made the decision not to eject. The Martin and Air Force teams who erected and tested the rocket found that some plugs on the rocket were able to pull out more easily than others. They replaced them with ones that were harder to pull out, and a safety wire was added to make sure that the rocket had lifted off. However, another problem was found as the engineers examined the thrust versus time graph. They found that the thrust rose nominally but started to decrease before the plug had fallen out. Through the night, engineers examined the rocket engine piece by piece until they found that a plastic cover had been left in the gas generator port. With this problem solved, the rocket and spacecraft were rescheduled for a launch three days after the first attempt. Rendezvous: The second attempt to launch the 6A mission (third attempt for Gemini spacecraft No. 6) was successful on December 15 at 8:37:26 a.m. EST. All went well through launch and ascent and the crew entered a 161 by 259 kilometers orbit, or as per the actual flight specifications, a 100 by 161 nautical mile orbit. The plan called for the rendezvous to take place on the fourth orbit of Gemini 6. Their first burn came 94 minutes after launch when they increased their speed by 5 meters per second, 16½ feet per second. Due to their lower orbit they were gaining on Gemini 7 and were only 730 miles, (or 1,175 kilometers), behind. The next burn was at 2 hours and 18 minutes when Gemini 6A made a phase adjustment to put them on the same orbital inclination as Gemini 7. They now only trailed by 483 kilometers, (300 miles). The radar on Gemini 6 first made contact with Gemini 7 at 3 hours and 15 minutes when they were 434 kilometers (270 miles) away. A third burn put them into a 168 x 170 mile (270 by 274 kilometer) orbit. As they slowly gained, Schirra put Gemini 6's computer in charge of the rendezvous. At 5 hours and 4 minutes he saw a bright star that he thought was Sirius, but this was in fact Gemini 7. After several more burns the two spacecraft were only 130 feet (40 meters) apart. The burns had only used 112 lbs. (51 kilograms) of fuel on Gemini 6, giving plenty of fuel for some fly-arounds. During the next 270 minutes the crews moved as close as 1 foot, (30 centimeters), talking over the radio. At one stage the spacecraft were stationkeeping so well that neither crew had to make any burns for 20 minutes. As the sleep periods approached, Gemini 6 made a separation burn and slowly drifted out to 10 miles (16 kilometers). This ensured that there would not be any accidental collisions in the night. A Christmas surprise: But before everyone went to sleep, the crew of Gemini 6 had a surprise for everyone: Gemini VII, this is Gemini VI_ We have an object, looks like a satellite going from north to south, up in a polar orbit. He's in a very low trajectory traveling from north to south and has a very high climbing ratio. It looks like it might even be a ... Very low. Looks like he mlght be going to reenter soon. Stand by one ... You might just let me try to pick up that thing. At that point, the sound of "Jingle Bells" was heard played on an 8-note Hohner "Little Lady" harmonica and a handful of small bells. The Smithsonian Institution claims these were the first musical instruments played in space and keeps the instruments on display. Reentry: Gemini 6 reentered the next day, landing within 18 kilometers (11 miles) of the planned site northeast of Turks and Caicos in the Atlantic Ocean, the first truly accurate reentry. It was also the first recovery to be televised live, through a transportable satellite earth station developed by ITT on the deck of the recovery aircraft carrier USS Wasp. The Gemini 7 and 6A missions were supported by the following U.S. Department of Defense resources: 10,125 personnel, 125 aircraft and 16 ships. Insignia: Walter Schirra explained the patch in the book All We Did Was Fly to the Moon: The Gemini 6 patch is hexagonal in shape, reflecting the mission number; and the spacecraft trajectory also traces out the number "6". The Gemini 6 spacecraft is shown superimposed on the "twin stars" Castor and Pollux, for "Gemini". I designed the patch to locate in the sixth hour of celestial right ascension. This was the predicted celestial area where the rendezvous should occur (in the constellation Orion). It finally did occur there. The original patch had called the flight GTA-6 (for Gemini-Titan-Agena) and showed the Gemini craft chasing an Agena. It was changed when the mission was altered to depict two Gemini spacecraft. Spacecraft location: The spacecraft is currently on display at the Oklahoma History Center in Oklahoma City, after having been on display at the Omniplex Science Museum elsewhere in the city. It is on a long term loan from the Smithsonian Institution. Before coming to Oklahoma, the spacecraft was displayed at the St. Louis Science Center in St. Louis, Missouri.Source: WikipediaText from this biography licensed under creative commons license